CN104991562A - Aircraft operating system, aircraft method control method and aircraft - Google Patents
Aircraft operating system, aircraft method control method and aircraft Download PDFInfo
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Abstract
The invention provides an aircraft operating system, an aircraft method control method and an aircraft. The operating system comprises a first memory cell used for storing aircraft factory configuration parameters; a second memory cell used for storing individual parameters set by users on an aircraft; a data exchange port used for exchanging data relevant to aircraft configuration with an external storage medium; a selection unit used for selecting parameters from the first memory cell and/or the second memory cell and/or the data exchange port; and a control unit used for updating parameters in the aircraft in dependence on the parameter information selected by the selection unit. Accordingly, in controlling different aircraft devices, only by inserting a portable storage medium into the data exchange port can a user rapidly select a suitable operation mode by debugging.
Description
Technical field
The present invention relates to the technical field of aviation aircraft, particularly relate to a kind of aircraft operating system, the control method of aircraft and aircraft.
Background technology
Along with the progress of electronic science and technology and the development of computer industry level, various types of aircraft progressively enters the sphere of life of people, such as in occasions such as some shooting, article transmission, demonstration flights, just often needs aircraft to perform corresponding task; Exactly because also there is this demand, the technology of aircraft is made to obtain good development.
Such as, be in the patented claim of CN201410187335.9 in Chinese Patent Application No., disclose a kind of double-layer spiral paddle multiple degrees of freedom four-axle aircraft, double-layer spiral paddle structure is positioned at the top of piggyback pod, vertical rotation controling mechanism is arranged at the side of piggyback pod and is connected with the output terminal of connecting rod, cam is controlled rotate and act on the course changing control structure be arranged in the middle part of fuselage main body by starter motor, this course changing control structure is rotated and is driven the steer motor bottom it, steer motor is connected with the input end of each connecting rod respectively and each piggyback pod and double-layer spiral paddle structure is freely rotated in surface level, such feature that can realize the overall flight attitude high flexible of flight, to adapt to the requirement for aircraft flight attitude under MODEL OVER COMPLEX TOPOGRAPHY.
Another part of Chinese Patent Application No. is in the patented claim of CN201210291738.9, disclose a kind of drive unit of double helix dish disc-shaped flying craft, by the turning operation system be located in aircraft cockpit, flight operation system and the driving mechanism composition be located at below double helix dish, wherein, flight operation system comprises flight balance control lever, operation bridge, bracing wire, flight fan blade deflecting roller, operation bridge lower end is fixed with an isosceles triangle framework, isosceles triangle framework two base angle is two spheroids, spheroid is provided with the groove for placing pull wire head, operation bridge is a Baltimore groove, Baltimore groove two ends are provided with the groove for holding two spheroids on fixing isosceles triangle framework, isosceles triangle framework is arranged on operation bridge by a control lever retracing spring, bracing wire one end is fixed on spheroid groove by pull wire head, the other end is connected with flight fan blade deflecting roller side, flight fan blade deflecting roller opposite side is connected with back-moving spring, flight fan blade deflecting roller is arranged on central shaft driving wheel motion flight air holes central shaft driving and is arranged on flight air holes central shaft, the stable performance of such aircraft, operating personnel can be very fast be familiar with associative operation, and fast easy to maintenance.
Inventor is realizing finding in process of the present invention: although the performance of aircraft self obtains well perfect in technique scheme, the operating performance of user have also been obtained improvement; But each user is when manipulating aircraft, all according to the difference of the feature of oneself health and operating habit, optimum configurations various in aircraft can be become adapt to the pattern of oneself flight; And user when completing aerial mission on different aircraft, all carry out parameter testing with regard to needs, and after may needing repeatedly to take a flight test at every turn, oneself parameter applicable could be debugged out; Therefore, aircraft of the prior art, is not well positioned to meet the comfort level that user manipulates aircraft, but also tuning parameter of will losing time.
Summary of the invention
In order to solve the above-mentioned problems in the prior art, the invention provides and a kind ofly can adapt to the aircraft operating system of user operation habits, a kind of control method of aircraft and a kind of aircraft fast.
Technical scheme provided by the invention is:
On the one hand, provide a kind of aircraft operating system, described aircraft is provided with the rotor that aircraft can be risen aloft, provides the motor of power to aircraft, sends the remote terminal of flight orders and perform the flight control panel of flight orders to aircraft; Described operating system comprises:
First storage unit, for store aircraft dispatch from the factory configuration default parameters;
Second storage unit, for storing the personalizing parameters that user is arranged on described aircraft;
Data switching port, for exchange to external storage media and aircraft arranges relevant data;
Selection unit, can carry out Selection parameter by described first storage unit and/or described second storage unit and/or described data switching port;
Control module, according to the parameter information that described selection unit is selected, upgrades parameter various in described aircraft.
Preferably, described external storage media can be chip card and/or release and/or USB interface equipment.
Preferably, described data switching port can replace with network communication unit and user account information administrative unit, and when user is after described user account information administrative unit logs in, described network communication unit exchanges various parameter information with outside.
Preferably, the parameter of described first cell stores is plaintext parameter, and the data that the personalizing parameters of described second cell stores and described data switching port receive are encryption parameters.
Preferably, the personalizing parameters of described second storage unit, can be stored in external storage media by described data switching port.
Preferably, described default parameters and/or personalizing parameters comprise user interface parameter, flight parameter and additional function parameter.
On the other hand, also provide a kind of control method of aircraft, described aircraft is provided with any one aircraft operating system above-mentioned, and described control method comprises:
1), aircraft and remote terminal is started;
2), Selection parameter is carried out by described first storage unit and/or described second storage unit and/or described data switching port;
3), by step 2) in select parameter be updated to control module.
Preferably, step 1) also comprises makes the network communication unit of aircraft network, step 2) also comprising can by user account information administrative unit Selection parameter.
Preferably, the control method of described aircraft also comprises and amended for user parameter is updated to described second storage unit and/or external storage media and/or user account information administrative unit.
The third aspect, also provides a kind of aircraft, and this aircraft comprises the rotor that aircraft can be risen aloft, provides the motor of power to aircraft, sends the remote terminal of flight orders and perform the flight control panel of flight orders to aircraft; And this aircraft also comprises any one aircraft operating system above-mentioned.
Adopt technique scheme, at least can have following beneficial effect:
(1) data about aircraft stored in foreign medium, can be received by data switching port, such user is when manipulating different flight equipments, only need portable storage medium to be inserted into data switching port, just can debug out oneself operator scheme applicable rapidly;
(2), user by user account information administrative unit and network communication unit, only need the account information logging in oneself, just directly can debug out oneself familiar parameter, make aircraft operation system more intelligent;
(3), the first cell stores expressly parameter, the second storage unit and data switching port receive encryption parameter, can more focus on individual subscriber privacy, and are beneficial to the experience achievement of protection user at flight domain;
(4), the amended personalizing parameters of user can pass through described data switching port, is stored in described external storage media; Or be updated to user account information administrative unit by network communication unit; Be convenient to the operating habit after user being upgraded in time like this preserve, when next user manipulates aircraft, automatically can be upgraded the operating habit of user by data switching port and/or network communication unit, improve the comfort level that user manipulates aircraft.
Accompanying drawing explanation
The structured flowchart of a kind of aircraft that Fig. 1 provides for the embodiment of the present invention one;
The structured flowchart of a kind of aircraft operating system that Fig. 2 provides for the embodiment of the present invention one;
Fig. 3 is the process flow diagram of the control method of a kind of aircraft that the embodiment of the present invention one was carried;
The structured flowchart of a kind of aircraft operating system that Fig. 4 provides for the embodiment of the present invention two;
The structured flowchart of a kind of aircraft operating system that Fig. 5 provides for the embodiment of the present invention three.
Embodiment
Below in conjunction with accompanying drawing, the specific embodiment of the present invention is described in detail, it should be noted that, these specific descriptions just allow those of ordinary skill in the art be more prone to, clearly understand the present invention, but not limitation of the invention is explained.
Embodiment one
As shown in Figure 1, embodiment one provides a kind of aircraft 1, comprise the rotor 2 that aircraft 1 can be risen aloft, the motor 3 of power is provided to aircraft 1, send the remote terminal 4 of flight orders to aircraft and perform flight control panel 5 and the electricity tune frame of flight orders, wherein, remote terminal 4 can be telepilot or the mobile device with remote control APP software; And comprise a kind of aircraft operating system 6, hereafter can be described in detail operating system.
Preferably, in the present embodiment, aircraft 1 is four-axle aircraft, and the physical construction of this aircraft can adopt double-layer spiral paddle multiple degrees of freedom four-axle aircraft of the prior art or double helix dish disc-shaped flying craft; And the image photographing device that can be provided with shoot function, cloud platform, central control unit (CPU) and information carrying means (network port).
As shown in Figure 2, embodiment one additionally provides a kind of aircraft operating system 6, and this operating system 6 comprises:
First storage unit 61, for store aircraft dispatch from the factory configuration default parameters;
Second storage unit 62, for storing the personalizing parameters that user is arranged on board the aircraft; Wherein, first storage unit 61 and the second storage unit 62 can be the storeies that in remote terminal 4, control chip carries, or the nonvolatile memory of control chip is connected to by expansion interface in control chip, control chip can also adopt single-chip microcomputer or FPGA to replace; And the first storage unit 61 and the second storage unit can be the zoness of different in same storer, can also be different storeies;
Data switching port 63, for exchange to external storage media and aircraft arranges relevant data;
Selection unit 64, can from the first storage unit and/or the second storage unit and/or data switching port Selection parameter; And selection unit 64 can be realized by the software switch on touch screen, or realized by the key up and down on remote terminal 4;
Control module 65, according to the parameter information that selection unit 64 is selected, upgrades parameter various in aircraft; Control module 65 can by the control chip of the single-chip microcomputer in remote terminal or other types or FPGA circuit, and the predetermined control program of burning realizes.
Preferably, external storage media can be chip card and/or release and/or USB interface equipment; Data switching port 63, then according to the difference of storage medium, is arranged to dissimilar port.
Preferably, the personalizing parameters of the second storage unit 62 can be stored in external storage media by data switching port 63.
Preferably, allocating default parameter of dispatching from the factory in above-mentioned first storage unit 61 comprises user interface parameter, flight parameter and additional function parameter; And the type of the default parameters that the data type of personalizing parameters that the second storage unit 62 stores and data switching port 63 receive in the type of data and the first storage unit 61 is identical.
Particularly, user interface parameter can be the parameter of following kind:
Be arranged on GPS locating information user's remote terminal showing current flight device, and by its real-time electronic chart shown.And the direction of electronic chart arranges and is usually divided into two kinds: a kind of is the basis that is oriented according to aircraft, keep aircraft on map towards being mode upwards all the time; Another kind is that according to the map based on data, mode map being remained up north and down south shows.These parameters can collect in the first storage unit 61, and the first storage unit 61 can be arranged to but be not limited to the storer in a kind of integrated chip.User interface parameter can also comprise languages (such as Chinese, English, Guangdong language, other dialects etc.), the sound type (such as male voice, female voice etc.) of voice message, the quantity of onscreen cue information and kind etc.
Flight parameter can be the parameter of following kind:
1, the lifting top in remote terminal, direction top, aileron and accelerator control method; Such as, for U.S.'s hand, (left hand controls throttle and yaw rudder, the right hand controls elevating rudder and aileron) (left hand controls elevating rudder and yaw rudder with Japanese hand, the right hand controls throttle and aileron), remote terminal of the prior art is the one supported wherein mostly, but along with the difference of user's use habit, in remote terminal, can realize the mode regulated and controled by software, change action type; In addition, along with the increase of number of users, even also start to occur more handling custom, such as " middle national champion ", i.e. left hand elevating rudder and aileron, right hand throttle and yaw rudder.In prior art, the user of a custom U.S. hand, if the aircraft needing manipulation is Japanese hand, so also need through a debug process, make this aircraft adapt to the manipulation custom of user, add the trouble of user, reduce the service experience of user; And adopt the technique scheme in the present embodiment, the operating habit of user is only needed to be stored in a kind of storage medium, then when user operation aircraft, storage medium is inserted above-mentioned data switching port 63, just can quickly move through above-mentioned selection unit 64 and control module 65, the remote terminal in aircraft is adjusted to the operator scheme of user oneself custom.
2, the remote control distance of aircraft, after the distance like this between aircraft body and remote terminal exceeds certain limit, will cause aircraft not receive remote signal, reduce unnecessary trouble.
Although different aircraft all may be provided with different mechanism to the situation avoiding the distance between aircraft body and remote terminal to exceed certain limit, such as, sense aircraft out of control after automatically make a return voyage, or aircraft reaches warning distance afterwards, does not just accept the instruction etc. far flown.But in the present embodiment, if user be Interim use aircraft to complete shoot function time, just can by less for the optimum configurations of this remote control distance, particularly, the personalizing parameters of user oneself can be adjusted by the second storage unit, such as in the situation of taking photo by plane, if user allows aircraft fly to take beyond 20 meters, shooting effect is now difficult to ensure; Can remote control distance be arranged to be less than 20 meters in advance, parameter adjustment can be passed through in advance like this, stop the not good phenomenon of shooting effect rapidly and occur.
Additional function parameter can be the parameter of following kind:
When using aircraft to complete other application functions, to the parameters of its external device.Such as, when completing aerial photography function with aircraft, the parameter of filming apparatus; Or when completing transportation function with aircraft, the parameter of chucking device.Particularly, to take photo by plane, carry-on capture apparatus acquiescence is in shooting portrait mode of figure, the parameters such as the continuous shooting interval under relevant time shutter, shutter parameter, automatically burst mode and continuous shooting number of times.
As shown in Figure 3, the present embodiment also provides a kind of control method of aircraft, and aircraft is provided with above-mentioned aircraft operating system, and this control method comprises:
S1, startup aircraft and remote terminal;
S2, Selection parameter type; By Selection parameter in the first storage unit and/or the second storage unit and/or data switching port, particularly, after each flight equipment or remote terminal electrifying startup, operating system can point out user to select the parameter configuration of wishing, these parameter configuration can be the allocating default parameters of dispatching from the factory stored in the first storage unit, also can be that user is stored into personalizing parameters in the second storage unit (on default parameters basis, according to the amended parameter of personal habits), can also be the data in the storage medium read from data switching port; Because the parameter stored in the first storage unit, the type that the personalizing parameters stored in the second storage unit and data switching port receive data is identical, so user can also select a part of parameter respectively from three kinds of parameters;
S3, renewal aircraft parameters; By step 2) in select parameter be updated to control module.
Adopt technique scheme, at least can have following beneficial effect:
(1) data about aircraft stored in foreign medium, can be received by data switching port, such user is when manipulating different flight equipments, only need portable storage medium to be inserted into data switching port, just can debug out oneself operator scheme applicable rapidly;
(2), the amended personalizing parameters of user can pass through data switching port, is stored in external storage media; To be convenient to like this to upgrade in time the operating habit of user, to improve the comfort level of user's manipulation.
Embodiment two
Embodiment two provides the control method of a kind of aircraft, aircraft operating system and aircraft equally.And aircraft is provided with the rotor 2 identical with embodiment one, provide the motor 3 of power to aircraft 1, send the remote terminal 4 of flight orders to aircraft and perform the flight control panel 5 of flight orders, and electricity adjusts frame; Difference is, the operating system 6 that embodiment two provides also comprises network communication unit 66 and user account information administrative unit 67, and when user is after user account information administrative unit 66 logs in, network communication unit 67 exchanges various parameter information with outside.Preferably, can receive the parameter information that user is debugged on different aircraft, these parameter informations can be stored on Cloud Server; Particularly, user can share at an internet and under the mechanism of maintaining secrecy, by aircraft or directly by the terminal such as computer, mobile phone realize to the aircraft use habit of individual and the network storage of parameter, when to need this data importing to the aircraft of current use in strange land, only needs realize strange land by this aircraft and download and import.
Preferably, the account in above-mentioned user account information administrative unit 67 can be specifically designed to the account of collecting aircraft user information parameter, and the user operation habits parameter of this account statistics, can be stored in network cloud server.
Preferably, the account in above-mentioned user account information administrative unit 67 can also be by account conventional in third-party platform, such as, can be conventional QQ account, micro-letter account, microblog account etc.; By these accounts, user can be allowed to exempt from registration, just can the operating habit of rapid saving oneself; And avoid puzzlements such as forgetting Password.
Preferably, second storage unit 62 is revised after parameter terminates user, user can be pointed out whether to preserve amended personalizing parameters, and by self-defined for preservation mode title, such user not only can call the last optimal operation mode, any operator scheme arranged before can also calling; Allow operating system hommization more.
Preferably, the control method of the aircraft that the present embodiment provides is on the basis of embodiment one, and step S1 also comprises makes the network communication unit 66 of aircraft network, and step S2 also comprises can by user account information administrative unit 67 Selection parameter.
Preferably, amended for user parameter, on the basis of embodiment one, is updated to the second storage unit and/or external storage media and/or user account information administrative unit by the control method of the aircraft that the present embodiment provides.
Adopt the technique scheme in the present embodiment, user can pass through user account information administrative unit 66 and network communication unit 67, only need the account information logging in oneself, just directly can debug out the parameter oneself be familiar with, make aircraft operation system more intelligent.
Embodiment three
As shown in Figure 5, embodiment three provides the control method of a kind of aircraft, aircraft operating system and aircraft equally.Difference is, data switching port, on the basis of embodiment one, is directly replaced with the network communication unit 66 in embodiment two and user account information administrative unit 67 by the present embodiment; The technical scheme that theres is provided of the present embodiment is provided, can plays equally in embodiment two by beneficial effect that user account information administrative unit 66 and network communication unit 67 obtain.
Embodiment four
Embodiment four is technical embodiment one and/or embodiment two, carries out rights management further to parameter various in aircraft:
Preferably, the parameter that the first storage unit 61 stores is plaintext parameter, and the personalizing parameters that the second storage unit 62 stores and the parameter that data switching port 63 receives are encryption parameters.Particularly, the parameter in the first storage unit 61 is read-only parameter, and any user can check; And the personalizing parameters that the second storage unit 62 stores and the data that data switching port 63 receives, in storage format, gauge outfit is all provided with ciphertext, and by predetermined cryptographic algorithm and other elements exchange information.
Therefore, in the aircraft control method that the present embodiment provides, if user is when step S2, when selecting the parameter in the second storage unit 62 or data switching port 63, need through decryption oprerations.And in the second storage unit 62 or data switching port 63 during write parameters, also need through decryption oprerations; Equally for when upgrading the parameter relevant to aircraft by login user name form, also need through decryption oprerations.
Adopt the technique scheme in the present embodiment, can more focus on individual subscriber privacy, and be beneficial to the experience achievement of protection user at flight domain.
Finally it should be noted that, above-mentioned explanation is only most preferred embodiment of the present invention, not does any pro forma restriction to the present invention.Any those of ordinary skill in the art; do not departing within the scope of technical solution of the present invention; the way of above-mentioned announcement and technology contents all can be utilized to make many possible variations and simple replacement etc. to technical solution of the present invention, and these all belong to the scope of technical solution of the present invention protection.
Claims (10)
1. an aircraft operating system, described aircraft is provided with the rotor that aircraft can be risen aloft, provides the motor of power to aircraft, sends the remote terminal of flight orders and perform the flight control panel of flight orders to aircraft; It is characterized in that, described operating system comprises:
First storage unit, for store aircraft dispatch from the factory configuration default parameters;
Second storage unit, for storing the personalizing parameters that user is arranged on described aircraft;
Data switching port, for exchange to external storage media and aircraft arranges relevant data;
Selection unit, can carry out Selection parameter by described first storage unit and/or described second storage unit and/or described data switching port;
Control module, according to the parameter information that described selection unit is selected, upgrades parameter various in described aircraft.
2. a kind of aircraft operating system as claimed in claim 1, is characterized in that, described external storage media can be chip card and/or release and/or USB interface equipment.
3. a kind of aircraft operating system as claimed in claim 1, it is characterized in that, described data switching port can replace with network communication unit and user account information administrative unit, when user is after described user account information administrative unit logs in, described network communication unit exchanges various parameter information with outside.
4. a kind of aircraft operating system as claimed in claim 1, it is characterized in that, the parameter of described first cell stores is plaintext parameter, and the data that the personalizing parameters of described second cell stores and described data switching port receive are encryption parameters.
5. a kind of aircraft operating system as claimed in claim 1, is characterized in that, the personalizing parameters of described second storage unit can be stored in external storage media by described data switching port.
6. a kind of aircraft operating system as claimed in claim 1, is characterized in that, described default parameters and/or personalizing parameters comprise user interface parameter, flight parameter and additional function parameter.
7. a control method for aircraft, described aircraft is provided with as the operating system of claim 1 ~ 6 as described in any one, and it is characterized in that, described control method comprises:
1), aircraft and remote terminal is started;
2), Selection parameter is carried out by described first storage unit and/or described second storage unit and/or described data switching port;
3), by step 2) in select parameter be updated to control module.
8. the control method of a kind of aircraft as claimed in claim 7, is characterized in that, step 1) also comprises makes the network communication unit of aircraft network, step 2) also comprising can by user account information administrative unit Selection parameter.
9. the control method of a kind of aircraft as claimed in claim 8, is characterized in that, also comprises and amended for user parameter is updated to described second storage unit and/or external storage media and/or user account information administrative unit.
10. aircraft comprises the rotor that aircraft can be risen aloft, provides the motor of power to aircraft, sends the remote terminal of flight orders and perform the flight control panel of flight orders to aircraft; It is characterized in that, described aircraft also comprises as claim 1 ~ 6 aircraft operating system as described in any one.
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| CN108445740A (en) * | 2018-03-21 | 2018-08-24 | 深圳臻迪信息技术有限公司 | Unmanned aerial vehicle (UAV) control method, non-transient computer readable storage medium and electronic equipment |
| WO2020042100A1 (en) * | 2018-08-30 | 2020-03-05 | 深圳市大疆创新科技有限公司 | Control method, system, device and computer readable storage medium |
| CN114138021A (en) * | 2021-11-29 | 2022-03-04 | 北京航空航天大学 | Multi-aircraft cluster privacy protection system and method under directed communication network |
| CN116320737A (en) * | 2023-05-10 | 2023-06-23 | 珠海星云智联科技有限公司 | Control method, equipment and medium for gigabit Ethernet standard industrial camera |
| CN116320737B (en) * | 2023-05-10 | 2023-08-18 | 珠海星云智联科技有限公司 | Control method, equipment and medium for gigabit Ethernet standard industrial camera |
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